JP6232148B2 - 飛行機、及びその信号線保護アセンブリ - Google Patents
飛行機、及びその信号線保護アセンブリ Download PDFInfo
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- JP6232148B2 JP6232148B2 JP2016568917A JP2016568917A JP6232148B2 JP 6232148 B2 JP6232148 B2 JP 6232148B2 JP 2016568917 A JP2016568917 A JP 2016568917A JP 2016568917 A JP2016568917 A JP 2016568917A JP 6232148 B2 JP6232148 B2 JP 6232148B2
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- landing leg
- protective sleeve
- signal line
- sleeve
- electronic governor
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- 230000001681 protective effect Effects 0.000 claims description 74
- 238000005491 wire drawing Methods 0.000 claims description 17
- 239000000853 adhesive Substances 0.000 claims description 13
- 230000001070 adhesive effect Effects 0.000 claims description 13
- 230000006378 damage Effects 0.000 claims description 9
- 238000010586 diagram Methods 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/52—Skis or runners
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/06—Undercarriages fixed
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/60—Oleo legs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
- H02G3/02—Details
- H02G3/04—Protective tubing or conduits, e.g. cable ladders or cable troughs
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
- H02G3/02—Details
- H02G3/04—Protective tubing or conduits, e.g. cable ladders or cable troughs
- H02G3/0406—Details thereof
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
- H02G3/02—Details
- H02G3/04—Protective tubing or conduits, e.g. cable ladders or cable troughs
- H02G3/0462—Tubings, i.e. having a closed section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D2221/00—Electric power distribution systems onboard aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Details Of Aerials (AREA)
- Casings For Electric Apparatus (AREA)
- Forklifts And Lifting Vehicles (AREA)
Description
Claims (12)
- 着陸脚と保護スリーブとを備え、前記着陸脚が着陸脚スリーブを備え、前記保護スリーブの少なくとも一部が前記着陸脚スリーブ内に収容され、前記保護スリーブが、信号線の外部環境による損壊を防止するように前記信号線を収容することに用いられ、
前記着陸脚スリーブは、載置プラットフォームと収容部とを備え、前記載置プラットフォームの一側面がプロペラを駆動するための動力システムの載置に用いられ、他側面に、前記保護スリーブを収容して固定させるための前記収容部が設けられることを特徴とする、飛行機における信号線保護アセンブリ。 - 前記保護スリーブと前記収容部との接触位置に接着剤が設けられ、前記接着剤により前記保護スリーブがさらに固定されることを特徴とする、請求項1に記載の信号線保護アセンブリ。
- 前記着陸脚は少なくとも二つであり、前記保護スリーブの両端がそれぞれ二つの前記着陸脚の着陸脚スリーブ内に収容され、前記保護スリーブに線引込み孔が設けられており、二つの前記着陸脚スリーブの載置プラットフォームには、前記保護スリーブの両端部のそれぞれ対応する位置に線引出し孔が設けられており、前記信号線が前記線引込み孔から前記保護スリーブ内に進入し、前記保護スリーブの端部から出て、さらに前記線引出し孔から前記動力システムに至るようになることを特徴とする、請求項1又は2に記載の信号線保護アセンブリ。
- 前記着陸脚に、さらに前記飛行機の電子調速機を収容する電子調速機室が設けられており、前記着陸脚スリーブの載置プラットフォームが前記電子調速機室に設けられると共に、前記保護スリーブが前記電子調速機室内に収容されるように、前記着陸脚スリーブの収容部が前記電子調速機室内に収容されることを特徴とする、請求項1〜3のいずれか一項に記載の信号線保護アセンブリ。
- 前記着陸脚は、着陸脚底蓋をさらに備え、前記着陸脚底蓋は、一端が前記電子調速機室の一端と接続されると共に、前記電子調速機室の下方に位置し、また、外部信号が受信できるアンテナを収容して、前記アンテナの外部環境による損壊を防止するように、前記着陸脚底蓋にアンテナチャンバーが設けられることを特徴とする、請求項4に記載の信号線保護アセンブリ。
- 保護スリーブには、前記電子調速機のデータ線と電源線、および前記アンテナのデータ線が収容されていることを特徴とする、請求項5に記載の信号線保護アセンブリ。
- 着陸脚と保護スリーブとを有する信号線保護アセンブリを備え、前記着陸脚が着陸脚スリーブを備え、前記保護スリーブの少なくとも一部が前記着陸脚スリーブ内に収容され、前記保護スリーブが、信号線の外部環境による損壊を防止するように前記信号線を収容することに用いられ、
前記着陸脚スリーブは、載置プラットフォームと収容部とを備え、前記載置プラットフォームの一側面がプロペラを駆動するための動力システムの載置に用いられ、他側面に、前記保護スリーブを収容して固定させるための前記収容部が設けられることを特徴とする、飛行機。 - 前記保護スリーブと前記収容部との接触位置に接着剤が設けられ、前記接着剤により前記保護スリーブがさらに固定されることを特徴とする、請求項7に記載の飛行機。
- 前記着陸脚は少なくとも二つであり、前記保護スリーブの両端がそれぞれ二つの前記着陸脚の着陸脚スリーブ内に収容され、前記保護スリーブに線引込み孔が設けられており、二つの前記着陸脚スリーブの載置プラットフォームには、前記保護スリーブの両端部のそれぞれ対応する位置に線引出し孔が設けられており、前記信号線が前記線引込み孔から前記保護スリーブ内に進入し、前記保護スリーブの端部から出て、さらに前記線引出し孔から前記動力システムに至るようになることを特徴とする、請求項7又は8に記載の飛行機。
- 前記着陸脚に、さらに前記飛行機の電子調速機を収容する電子調速機室が設けられており、前記着陸脚スリーブの載置プラットフォームが前記電子調速機室に設けられると共に、前記保護スリーブが前記電子調速機室内に収容されるように、前記着陸脚スリーブの収容部が前記電子調速機室内に収容されることを特徴とする、請求項7〜9のいずれか一項に記載の飛行機。
- 前記着陸脚は、着陸脚底蓋をさらに備え、前記着陸脚底蓋は、一端が前記電子調速機室の一端と接続されると共に、前記電子調速機室の下方に位置し、また、外部信号が受信できるアンテナを収容して、前記アンテナの外部環境による損壊を防止するように、前記着陸脚底蓋にアンテナチャンバーが設けられることを特徴とする、請求項10に記載の飛行機。
- 保護スリーブには、前記電子調速機のデータ線と電源線、および前記アンテナのデータ線が収容されていることを特徴とする、請求項11に記載の飛行機。
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2014/080845 WO2015196418A1 (zh) | 2014-06-26 | 2014-06-26 | 一种飞行器及其信号线保护组件 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2017516699A JP2017516699A (ja) | 2017-06-22 |
JP6232148B2 true JP6232148B2 (ja) | 2017-11-15 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2016568917A Active JP6232148B2 (ja) | 2014-06-26 | 2014-06-26 | 飛行機、及びその信号線保護アセンブリ |
Country Status (5)
Country | Link |
---|---|
US (4) | US9896195B2 (ja) |
EP (2) | EP3162704B1 (ja) |
JP (1) | JP6232148B2 (ja) |
CN (1) | CN104755371B (ja) |
WO (1) | WO2015196418A1 (ja) |
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-
2014
- 2014-06-26 EP EP14896036.2A patent/EP3162704B1/en not_active Not-in-force
- 2014-06-26 WO PCT/CN2014/080845 patent/WO2015196418A1/zh active Application Filing
- 2014-06-26 EP EP19152781.1A patent/EP3509172B1/en active Active
- 2014-06-26 JP JP2016568917A patent/JP6232148B2/ja active Active
- 2014-06-26 CN CN201480002728.6A patent/CN104755371B/zh active Active
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2016
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2017
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EP3162704A4 (en) | 2017-06-07 |
EP3509172B1 (en) | 2022-03-16 |
EP3162704A1 (en) | 2017-05-03 |
EP3509172A1 (en) | 2019-07-10 |
US11180246B2 (en) | 2021-11-23 |
US9896195B2 (en) | 2018-02-20 |
US10513329B2 (en) | 2019-12-24 |
US20180086441A1 (en) | 2018-03-29 |
JP2017516699A (ja) | 2017-06-22 |
CN104755371B (zh) | 2016-08-31 |
US20200148341A1 (en) | 2020-05-14 |
US20170113789A1 (en) | 2017-04-27 |
CN104755371A (zh) | 2015-07-01 |
US20190202552A1 (en) | 2019-07-04 |
US10227131B2 (en) | 2019-03-12 |
EP3162704B1 (en) | 2019-03-06 |
WO2015196418A1 (zh) | 2015-12-30 |
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